The Effects Of Sideslip Aspect Ratio And Mach Number On The Lift And Pitching Moment Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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The Effects Of Sideslip Aspect Ratio And Mach Number On The Lift And Pitching Moment Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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Author : Arthur L. Jones
language : en
Publisher:
Release Date : 1949
The Effects Of Sideslip Aspect Ratio And Mach Number On The Lift And Pitching Moment Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur L. Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerofoils categories.
The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.
The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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Author : Arthur Leslie Jones
language : en
Publisher:
Release Date : 1949
The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur Leslie Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Supersonic categories.
The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.
Some Theoretical Characteristics Of Trapezoidal Wings In Supersonic Flow And A Comparison Of Several Wing Flap Combinations
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Author : Robert O. Piland
language : en
Publisher:
Release Date : 1951
Some Theoretical Characteristics Of Trapezoidal Wings In Supersonic Flow And A Comparison Of Several Wing Flap Combinations written by Robert O. Piland and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aerodynamics, Supersonic categories.
The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force and yawing moment due to rolling of a trapezoidal wing are derived. The equations are applicable when the inboard Mach line from a leading-edge tip intersects the trailing edge and the outboard Mach line lies ahead of the side edge. When the side edges are raked in, the former condition is sufficient. A comparison based on theoretical expressions of the lift and rolling effectiveness for half-delta tip (point forward) and trailing-edge flaps on various plan forms is made.
Bibliography Of Technical Reports
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Author :
language : en
Publisher:
Release Date : 1950
Bibliography Of Technical Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Science categories.
Investigation Of The Effects Of Model Scale And Stream Reynolds Number On The Aerodynamic Characteristics Of Two Rectangular Wings At Supersonic Speeds On The Langley 9 Inch Supersonic Tunnel
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Author : Donald E. Coletti
language : en
Publisher:
Release Date : 1955
Investigation Of The Effects Of Model Scale And Stream Reynolds Number On The Aerodynamic Characteristics Of Two Rectangular Wings At Supersonic Speeds On The Langley 9 Inch Supersonic Tunnel written by Donald E. Coletti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aerodynamics, Supersonic categories.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1950
Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aeronautics categories.
Technical Note
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1950
Technical Note written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aeronautics categories.
Application Of The Laplace Transformation To The Solution Of The Lateral And Longitudinal Stability Equations
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Author : Andrew Gustav Mokrzycki
language : en
Publisher:
Release Date : 1950
Application Of The Laplace Transformation To The Solution Of The Lateral And Longitudinal Stability Equations written by Andrew Gustav Mokrzycki and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Airplanes categories.
The application of the Laplace transformation to the solution of the lateral and longitudinal stability equations is presented. The expressions for the time history of the motion in response to a sinusoidal control motion are derived for the general case in which the initial conditions, initial displacements and initial velocities, are assumed different from zero. Some illustrative examples of the application of the Laplace transform to ordinary linear differential equations with constant coefficients and a number example of a specific problem are presented in appendixes.
The Rolling Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow
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Author : Arthur L. Jones
language : en
Publisher:
Release Date : 1948
The Rolling Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur L. Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aerodynamics, Supersonic categories.
The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.
Aero Digest
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Author :
language : en
Publisher:
Release Date : 1950
Aero Digest written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aeronautics categories.